发明名称 COMPRESSOR BLADES
摘要 An improved thin, plate-like, compressor blade having stiffening ribs on its airfoil surfaces extending from or adjacent the leading edge of the blade toward the trailing edge and being positioned on the blade to reduce the tendency of the blade to fail by buckling when the leading edge of the blade is struck by foreign objects.
申请公布号 US3706512(A) 申请公布日期 1972.12.19
申请号 USD3706512 申请日期 1970.11.16
申请人 UNITED AIRCRAFT OF CANADA LTD. 发明人 ARTHUR D. STRELSHIK
分类号 F04D21/00;F04D29/32;(IPC1-7):F01D5/10 主分类号 F04D21/00
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